A grid interfacing zonal algorithm for three-dimensional transonic flows about aircraft configurations
Author:
Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/3-540-11948-5_7.pdf
Reference9 articles.
1. Boppe, C. W., and Stern, M. A.: “Simulated Transonic Flows for Aircraft with Nacelles, Pylons, and Winglets,” AIAA Paper 80-0130,1980.
2. Shankar, V., and Malmuth, N. D.: “Computational and Simplified Analytical Treatment of Transonic Wing-Fuselage-Pylon-Store Interactions,” AIAA Paper 80-0127,1980
3. Srokowski, A. J., Shrewsbury, G. A., and Lores, M. E.: “A Transonic Mutual Interference Program for Computing the Flow about Wing-Pylon/Nacelle Combinations”, AIAA Paper 80-1333,1980.
4. Yu, N. J.: “ Transonic Flow Simulation for Complex Configurations with Surface Fitted Grids,” AIAA Paper 81-1258, 1981.
5. Holst, T., and Thomas, S.: “Numerical Solution of Transonic Wing Flow Fields,” AIAA Paper 82-0105, 1982.
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